Aircraft cargo loading logistics system

Abstract

A cargo loading logistics system for verifying cargo loaded on an aircraft receives a desired restraint configuration from a database and determines an actual restraint configuration on the aircraft by receiving data from a plurality of machine readable identifiers corresponding to a plurality of install points and data from a plurality of machine readable identifiers corresponding to a plurality of restraints. The cargo loading logistics system then compares the desired restraint configuration with the actual restraint configuration and determines if the aircraft is properly configured to be loaded for an upcoming flight.

Description

FIELD OF THE INVENTION [0001] The present invention is directed to a system for assisting cargo aircraft. More particularly, it is directed to a cargo loading system for cargo aircraft. BACKGROUND INFORMATION [0002] With the increasing emphasis on packages, mail, and other such items having to arrive at its location “overnight”, more and more cargo is being shipped by aircraft 100 (See FIG. 1). While some aircraft are configured to transport cargo only, others are configured to transport both passengers and cargo. [0003] Typically, the items being shipped are first loaded onto pallets, containers, or the like. In the airfreight industry, any one of these various categories of devices is referred to as a Unit Load Device 102 (ULD). Within each category, the ULDs come in various sizes, shapes and capacities and bear markings 104 that identify their type, maximum gross weight and tare weight, among other characteristics. [0004] This initial task of placing the items to be shipped into ...

AI Technical Summary

Benefits of technology

[0015] In one aspect, the present invention is directed to a database comprising information associated with cargo restraints installed in one or more cargo compartments of an aircraft. Such a database includes first identifying information associated with a location of each of a first plu

Problems solved by technology

However, not all install points are populated with restraints, due to the weight and cost of the latter.

An overloaded or improperly balanced aircraft will require more power and greater fuel consumption to maintain flight, and the stability and controllability may be seriously affected.

Lack of appreciation for the effects of weight and balance on the performance of aircraft, particularly in combination with such performance reducing factors as high density altitude, frost or ice on the wings, low engine power, severe or uncoordinated maneuvers, and emergency situations, can be a prime factor in aircraft accidents.

During the inspection process, the loading crew member may discover a missing, damaged, or inoperable restraint.

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